JASC 7200
Service difficulty reports · 14,730
Reports filed under 7200 · Engine (Turbine/Turboprop), newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '7200' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '7200' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASAA2016012314971Engine · faultedWHILE PERFORMING T/C 78273000, FOUND NR 1 ENGINE FAULT MSG 73-31371, UPPER EGT SECTORS READING HIGH ON FLIGHT LEG 2 ECONOMIC FAULT. ACFT GROUNDED. ON DEFERRAL.SDR HALA2016012200013Engine · cokedDUCT ODOR, CONTINUED STRONG ODOR. SEEMS LIKE A/C PACK DUCT ISSUE THROUGHOUT CABIN. NO ASSOCATED MESSAGES, ECAM. PORT IP3S, EVIDENCE OF COKING. R & R NR 2 ENGINE IAW AMDS WC 7100-9401-02.SDR HALA20160122013Engine · cokedON APP, CONTINUED STRONG ODOR "DUCT SMELL", OPINION, SEEMS LIKE A/C PAX DUCT ISSUE THROUGHOUT CABIN NO ASSOCIATING MESSAGE,ECAM. PRELIMINARY INSPECTION IS A FINDING OF OIL AND COKING AROUND THE 3RD AND 4TH STAGE IP ROTORS. FERRIED ACFT FOR NR 2 ENGINE
CHANSDR CA160203005Engine · unknown(CAN) IT WAS REPORTED THAT THE CREW OF ABOVE ACFT MADE A TURNBACK TO ORIGIN AIRPORT AFTER EXPERIENCING AN OIL ODOR FROM THE BLEED/PRESSURIZATION SYS. ONCE ON THE GROUND, THEY ISOLATED THE ODOR TO THE RT ENGINE CABIN BLEED. TROUBLESHOOTING IS ON-GOING.SDR CA160203003Engine · power loss(CAN) DURING CRUISE, THE ENGINE HAD A POWER ROLL BACK AND THE PILOT WAS NOT ABLE TO RECOVER POWER VIA POWER LEVER (PLA) COMMAND. ELECTED TO RETURN TO HIS DEPARTURE POINT WHERE AN UNEVENTFUL LANDING WAS MADE. AFTER THE EVENT THE ENGINE WAS STARTED AND IT TOOK SDR CA160203016Engine · power loss(CAN) WHILE THE ACFT WAS RETURNING FOR LANDING AFTER CROP-DUSTING FLIGHT, THE ENGINE POWER DROPPED AND REMAINED AT IDLE. THE PILOT PERFORMED A PRECAUTIONARY LANDING IN A PASTURE AREA. ACFT SUSTAINED NO DAMAGED AND THE PILOT WAS NOT INJURED.SDR ASAA2016011614839Engine · malfunctionedNEGATIVE START NR 1 ENGINE, 25 PERCENT MAX MOTORING NO EGT WITH RT IGNITION SECOND START NEGATIVE START ENGINE 1, 25 PERCENT MAX MOTORING NO EGT WITH LT IGNITION. ACFT GROUNDED. PERFORMED FIM 74-21, TASK 807 ON NR 1 ENGINE. APPLIED HEAT TO COLD SOAKED ENGINE. SDR CA160121007Engine · odor(CAN) MINOR OIL FUMES WERE DETECTED IN THE COCKPIT AFTER START. ODOR ISOLATED TO NUMBER 1 ENGINE SIDE. AIRCRAFT WAS SHUT DOWN AND DECLARED UNSERVICEABLE. TROUBLESHOOTING LED TO THE REPLACEMENT OF THE HANDLING BLEED VALVE SOLENOID, AIR CONDITIONING UNITS WERE CSDR ANCF2016011202Engine · bird ingestionDURING TAKEOFF RNWY 34, SKCC ENG NR 2 HAD THE STRIKE, N1 INCREASED UP TO 4,7 VIB WHILE N2 VIB REMAINED UNCHANGED. PARAMETERS WERE LOOKED IN QRH PAGE 70,09A & NOT EXCEED THOSE VLVS. IAW AMM 05-51-19-200-601A INSPECTION OF THE ENG AFTER A BIRD STRIKE OR SLUSH SDR WX0A201601213069Engine · stalledDURING CLIMB NR 2 ENGINE HAD COMPRESSOR STALLS. PERFORMED QRH 72.8, STALLS STOPPED, CONTINUED FLIGHT. NR 2 ENGINE HAD LOW EPR & N1W & HIGH EGT & EQUAL N2. R & R RT ENGINE.SDR ASAA2016011114736Engine · faultedWHILE ACCOMPLISHING TASK CARD 78273000, NR 2 ENGINE RECENT FAULT SHOWS FAULT MSG NR 73-21442, DEU2 DATA IS MISSING. ACFT GROUNDED. ACCOMPLISHED FIM TASK 73-24, TASK 815 E, 1, A. MSG 73-21442 NOT ACTIVE. ELECTRONIC ENGINE CONTROL TEST PASSED, NO FAULTS FOUNDSDR R61A201601110060Engine · failedF/A REPORTED SMOKE IN THE CABIN. CREW DECLARED AN EMERGENCY, RETURNED TO DEPARTURE AND WITH EMERGENCY VEHICLES ROLLING, LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND OIL ALL OVER THE COMPRESSOR CASE. MAINTENANCE R & R ENGINE NR 2 IAW AMM AND OPS SDR ASAA2016011014722Engine · hung startHUNG START, NR 1 ENGINE INDICATION, N1 AND N2 FUEL FLOW NO EGT, ABORTED START FOLLOWED QRC PROCEDURES IGNITION SWITCH IN THE RT POSITION. ACFT GROUNDED. REMOVED NR 1 ENGINE RT IGNITION LEAD AND INSPECTED, CHECKS NORMAL. REINSTALLED IGNITION LEAD REF AMM 74-SDR FDEA201601100105Engine · bird ingestionMULTIPLE FAN BLADES DAMAGED ON NR 3 ENG DUE TO BIRD STRIKE. DURING BORESCOPE OF NR 3 ENG FOR BIRD STRIKE, FOUND LARGE TEAR ON LE 10TH STAGE THROUGH PORT B1-10. REPLACED NR 3 ENG.SDR ASAA2016010814704Engine · faultedWHILE ACCOMPLISHING T/C 78273000 FOUND NR 2 ENGINE ECONOMIC FAULT 73-31372, UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. ON DEFERRAL.SDR ASAA2016010814703Engine · faultedIAW T/C 78273000, FOUND NR 1 ENGINE WITH ECONOMIC FAULT 73-31371. UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. ON DEFERRAL.SDR CA160121001Engine · failed(CAN) DURING FLIGHT, THE CREW SAW THE LT ENGINE OIL PRESSURE DROP TO ZERO FOLLOWED BY A LOW OIL PRESSURE WARNING. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED AT DESTINATION. POST FLIGHT INSPECTION FOUND NO EVIDENCE OF EXTSDR CA160120013Engine · power loss(CAN) DURING TAKEOFF, THAT ACFT IS REPORTED TO HAVE SUFFERED A POWER LOSS BEFORE IT CRASHED IN A DITCH JUST OFF THE RUNWAY. A POST-CRASH FIRE OCCURRED. BOTH CREW MEMBERS WERE INJURED AND TRANSPORTED TO THE HOSPITAL. NO FURTHER DETAILS ARE AVAILABLE AT THIS TISDR CA160120002Engine · power loss(CAN) DURING TAKEOFF, THAT ACFT IS REPORTED TO HAVE SUFFERED A POWER LOSS BEFORE IT CRASHED IN A DITCH JUST OFF THE RUNWAY. A POST-CRASH FIRE OCCURRED. BOTH CREW MEMBERS WERE INJURED AND TRANSPORTED TO THE HOSPITAL. NO FURTHER DETAILS ARE AVAILABLE AT THIS SDR CA160120003Engine · overtorqued(CAN) PILOT WAS PERFORMING TOUCH AND GO EXERCISES AND WHILE PERFORMING A GO AROUND, THE ENGINE REVERTED TO MANUAL MODE. PILOT RETURNED TO POINT OF ORIGIN AND LANDED SAFELY. THE PMU DATA ANALYSIS REVEALED THE ENGINE HAD AN OVER TORQUE Q, LIMIT OF 132.78 PERCESDR CA160119023Engine · shutdown(CAN) CREW REPORTED GENERATOR FAILURE, AIRFRAME PART, DURING FLIGHT. IT WAS FIXED BY RESETTING THE CIRCUIT BREAKER. AFTER LANDING, WHILE TAXING, THE LT ENGINE SHUTDOWN WITH NO WARNING LIGHT OR OTHER INDICATIONS. THE CREW NOTICED THE TORQUE AND OIL PRESSURE ISDR SWIA201641721Engine · failedAFTER TAKING OFF AND CLIMBING THRU FL 600 THE CREW HEARD A THUMP AND THE NR 1 ITT STARTED FLASHING RED FOLLOWED BY AN ENGINE VIBRATION. CREW SHUT THE ENGINE DOWN AND RETURNED TO DEPARTURE. CREW DECLARED AN EMERGENCY. THE EXCEEDANCE PAGE OF THE MDC SHOWED THESDR AALA20160104010Engine · failedENGINE NR 2 CONTINUAL COMPRESSOR STALLING ON LIFT OFF. LOSS OF EPR, LOUD REPORTS & FLASHING. KEPT ENG NR 2 IN IDLE POSITION & FLEW LT CIRCUIT BACK TO RUNWAY 31L. AN EMER WAS DECLARED. AARF REPORT ON RUNWAY THAT NR 2 ENG SHOWING SMOKE. ENG WAS SHUT DOWN DUSDR GTIA2015010301444Engine · odorON APPROACH, AT ABOUT 10K FT, BOTH PILOTS DETECTED SIGNIFICANT ODOR OF DIRTY SOCKS OR SOUR MILK. SUSPECTING POSSIBLE PACK FUME EVENT, WE TURNED OFF PACK 1 TO ISOLATE AND ODOR INSTANTLY WENT AWAY. TROUBLESHOT IAW TSM 05-50-00-810-831A. IAW DECISION TABLE, ODOSDR U5QA201601060074Engine · malfunctionedPASSING 12,300', EXPERIENCED A LOUD BANG & SHUTTER FROM LT ENG. LT ENG VIB, AMBER CAS ILLUMINATED. POWER REDUCED TO IDLE, ENG VIB CAS EXTINGUISHED BUT SIGNIFICANT VIBRATION FELT IN CONTROLS. ELECTED TO DIVERT DUE TO WX & ACFT WEIGHT. POST FLIGHT INSPECTIONSDR WX0A2016010473061Engine · failedFLIGHT 145 WAS AT CRUISE AT FL330. THEY HEARD A BANG & FELT A SHUDDER IN THE ACFT. THEY WATCHED THE RT ENG INDICATIONS ROLL BACK AS THE ENG SHUTDOWN & RT ENG EGT MAXED OUT AT 800 DEGREES. DECLARED AN EMER & STARTED A DESCENT WITHIN LESS THAN A MINUTE OF THESDR CA160119016Engine · stalled(CAN) THE ENGINE STARTED STALLING DURING TAXI, ENGINE TEMPERATURE, ITT, WENT UP AND THE PILOT SHUTDOWN THE ENGINE. THE ENGINE WOULD NOT START. THE DATA DOWNLOAD SHOWS AN ITT EXCEEDANCE ON THE LT ENGINE. TROUBLESHOOTING IS ON-GOING.SDR WX0A2015123173057Engine · failedACFT HAD A SUDDEN ENG FAILURE AT CRUISE AT FL320. AN EMER WAS DECLARED, THE ENG WAS SECURED & THE CREW LANDED. THE PAXS DID NOT BRACE. THIS ACFT WAS ABOUT 500 POUNDS OVERWEIGHT FOR THE LANDING. THE RT ENG SPOOLED DOWN WITHOUT ANY WARNING. THE ONLY OTHER CSDR CALA2016010400010Engine · malfunctionedDURING ATTEMPTED NR 1 ENG START, ENG STARTED & OVERTEMPED AT 577 UNTIL TOLD WE HAD AN ENG TAIL PIPE FIRE. NO FIRE WARNING IN COCKPIT. DISCHARGED NR 1 ENG NR 1 BOTTLE. NEW ENG INSTALLED. SEE WC 19-7100-1-0900 DEC 31 2015 FOR DETAILS.SDR CA160119021Engine · malfunctioned(CAN) THE OPERATOR REPORTED THAT 4 TIMES OUT OF 5, THE ENGINE WILL NOT GO IN REVERSE. CYCLING THE CONTROLS HAD NO EFFECT. TROUBLESHOOTING IS ON-GOING WITH RIGGING TESTING AND PROPELLER GOVERNOR SWAP.SDR ASAA2015123014617Engine · vibrationDIAGNOSTICS REPORTS THE NR 1 ENGINE HAS EXPERIENCED A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. PEAKING AT 2.56 UNITS DURING CLIMB. VIBRATION LEVELS PRIOR TO INCREASE WERE STABLE AT 0.6 UNITS. ACFT GROUNDED. ACCOMPLISHED AMM TASK 71-00-00-800-SDR DALA2016010100017Engine · malfunctionedFAS IN AFT CABIN REPORTED POPS FROM LT ENGINE AT TAKEOFF POWER. REPLACED NR 1 ENGINE IAW 88-7110-9-0010.SDR AALA201512299001Engine · failedAIRCRAFT WAS GNDED. ENG NR 1 STALL ECAM 2 TIMES. NO FLUCTUATIONS N1, N2, EGT NORMAL. FLIGHT LEVEL 370 WITH THRUST REDUCTION. NR 1 ENG FAILED BORESCOPE & WAS REPLACED IAW TASK CARD 26L40071001.SDR FDEA201512284090Engine · power lossDURING DESCENT BELOW PROFILE THRUST WAS APPROX 75 - 77% N1. AT PROFILE THROTTLES REDUCED TO IDLE & APPROX 60% N1, A THUMPING SOUND WAS HEARD & FELT. SUSPECT COMPRESSOR STALL. ALTITUDE 30000 FT SPEED 0.8. NO ABNORMAL ENG INDICATIONS. SUSPECT ENG NR 2. SDR SWIA201541705Engine · flamed outDURING DEPARTURE, ENCOUNTERED MODERATE TO SEVERE TURBULENCE. HEARD TRIPLE CHIME "ENGINE OIL" WITH POSSIBLE FLAMEOUT. LT ENGINE SPOOLED DOWN SLIGHTLY, ENGAGED CONTINUOUS IGNITION AND ENGINE THRUST RESTORED. ALSO, HAD STICK SHAKER IN NORMAL CLIMB ATTITUDE, ISDR CA160119014Engine · shutdown(CAN) THE OPERATOR REPORTED AN ENGINE UNCOMMANDED SHUTDOWN ON GROUND SHORTLY AFTER LANDING. THIS HAPPENED AFTER THE PILOT DID 2 POWER MANAGEMENT SYSTEM (PMS) RESET`S DUE TO POWER MANAGEMENT UNIT, PMU FAULT. THE FLIGHT DATA SHOWED THAT THE PILOT DID RESET THE PSDR SWAA2015122947459Engine · failedAIR RETURN, INFLIGHT SHUTDOWN. NR 2 ENG LOUD BANG & SHUTDOWN. R & R NR 2 ENG IAW MT.SDR ASAA2015122314469Engine · faultedNR 2 ENGINE HAS RECENT FAULT 73-31372 UPPER EGT SECTORS READ HIGH, ECONOMIC FAULT. ACFT GROUNDED.SDR CA151229006Engine · leaking(CAN) THE OPERATOR REPORTED THAT UPON DEPARTURE THAT THE CABIN FILLED WITH OIL MIST. THE ACFT RETURNED TO THE POINT OF DEPARTURE. GROUND INSPECTION OF THE ACFT FOUND OIL IN THE LT BLEED DUCT.SDR CA151229005Engine · overtemp(CAN) THE OPERATOR REPORTED THAT ITT EXCEEDANCE OCCURRED DURING TAXI-OUT TO MISSION. THE ACFT TAXIED BACK TO GATE. AFTER COOL-DOWN, ENGINE HUNG-STARTS.SDR CA151228009Engine · power loss(CAN) DURING TAKEOFF ROLL, THE PILOT NOTICED A LOSS OF TORQUE (ONLY GETTING 1100 TO 1200 FT-LB). THE ENGINE THEN SHUT DOWN AND THE PROPELLER FEATHERED. HE ABORTED TAKEOFF AND THE AIRCRAFT STOPPED ON THE FAR RUNWAY THRESHOLD. HE GOT OUT OF THE AIRCRAFT, EXAMINESDR AALA20160113004Engine · leakingAIRCRAFT WAS GNDED. DURING FLIGHT BURNT SOCK SMELL REPORTED IN CABIN. SMELL DISSIPATED, THEN RETURNED WHEN RT PACK WAS TURNED OFF THE ON. FOUND SOURCE OF SMELL TO BE FROM NR 2 ENG DUE TO OIL WETTING BEHIND FAN BLADES. R & R NR 2 ENG IAW MCM CARD 71-94-01. SDR HALA2015121800250Engine · malfunctionedETOPS SIGNIFICANT SYSTEM, IN CRUISE FL370 STATUS MESSAGE RT OIL FILTER 2 MINUTE LATER RT OIL FILTER EICAS MSG ILLUMINATED, RETARDED RT ENGINE LEVER PROGRESSIVELY UNTIL EICAS OUT IAW QRH PROCEDURE EICAS WOULD ILLUMINATE UNTIL POWER REDUCED TO FOLLOWING SETTINGSSDR AALA201512199001Engine · bird ingestionAIRCRAFT WAS GNDED. DURING TAKEOFF ENCOUNTERED BIRD STRIKE. FOLLOWED BY RT ENG VIBRATION, LOW OIL PRESS & ENG FIRE WARNING. SHUT RT ENG DOWN. RETURNED TO FIELD. R & R RT ENG IAW JC 33L40071003.SDR CA151229010Engine · malfunctioned(CAN) WHILE CLIMBING OUT AT APPROXIMATELY 4000 FT WITH THRUST SET IN THE CLIMB DETENT, THE LT ENGINE EXPERIENCED A REDUCTION IN THRUST IN CONJUNCTION WITH LT ELECTRONIC ENGINE CONTROL ANNUNCIATION. THE PILOT ELECTED TO DO A DIVERSION AND LANDING AT HOME BASE.SDR CA151228008Engine · malfunctioned(CAN) UPON REACHING CRUISING ALTITUDE AT FL 240, BOTH POWER LEVERS, PLA, WERE REDUCED TO 52 PERCENT. THE CREW NOTICED THAT ENGINE NR 2 TORQUE DROPPED TO 12 PERCENT. THEY ADVANCED PLA RIGHT AWAY AND ENGINE RESPONDED, TORQUE COME BACK TO NORMAL. ENGINE OPERATEDSDR QXEA2015121500648Engine · odorDESCENT THROUGH APROXIMATELY 130000" FOR LANDING. F/A REPORTED SMOKE IN THE CABIN. DECLARED EMERGENCY, RAN CHECK LIST. SMOKE CONTINUED TILL EVACUATION, ON RUNWAY. ENGINE POWER WAS APPROXIMATELY 20 PERCENT TORQUE. BLEED AUTO ICE PROTECTION ON. ACFT CURRENTSDR CA151228007Engine · smoke(CAN) WHILE LANDING ON A TRAINING FLIGHT, AFTER THE REVERSE WAS APPLIED AND STOWED NORMALLY, THE LT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. THE PILOT TRIED TO INCREASE POWER BUT NO RESPONSE. WHITE SMOKE COULD BE SEEN LEAVING THE COWLING AFT AND EXHAUST. ESDR CALA2015121300994Engine · malfunctionedRIGHT ENG OIL PRESS 0, SHUT DOWN RT ENG. THE OIL PRESS LIGHT CAME ON DURING THE CLIMB. LEVELED OFF, SHUT DOWN & RETURNED. ENG SHUT DOWN FOR 20 MIN. R & R NR 2 ENG IAW WC 19-7100-1-0900 SEQ 10, RAN ENG OPERATIONS CHECKED NORMAL, NO LEAKS NOTED. ROTABLE PARSDR CA151228003Fadec · unknown(CAN) THE CUSTOMER REPORTED AN ENGINE #2 IFSD ON TRANSITION TO THE TAXIWAY WITH A NOISE OBSERVED (ITT 500) AND A NO DISPATCH MESSAGE. CREW OBSERVED FADEC FAULT CODES: 2A-AF-IGV AND 2B-AH-IGV (ACTUATOR). TROUBLESHOOTING ONGOING.
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